期刊文献+

高效双压氦液化循环研究 被引量:2

Research on efficient double-pressure helium liquefaction cycle
原文传递
导出
摘要 为了实现氦液化系统的高效性,提出了一种新型双压氦液化循环,探索在相同的高压压力下,流程参数、部件效率、系统液化率及(火用)效率等重要参数随中压压力的变化规律.结果表明:改变中压压力,流程液化率随着中压压力的增加而增加,而(火用)效率随之减小,当中压压力为7.0×10^(5)Pa时,液化量为90.46 L/h,(火用)效率达到最大值18.6%,当中压压力为12.5×10^(5)Pa时,液化量和(火用)效率分别为107.4 L/h和17.5%;双压氦液化循环相较于modified-Claude(修正-克劳德)循环,减小了节流阀处的损失,同时降低了系统功耗,提高了系统整体的(火用)效率. To realize the high-efficiency of helium liquefaction system,a new double-pressure helium liquefaction cycle was proposed to explore the law of main performance parameters such as process thermodynamic parameters,component efficiency,system liquefaction rate and exergy efficiency with medium pressure under the same high pressure.Results show that when the medium pressure is changed,the liquefaction rate increases with the increase of medium pressure,while the exergy efficiency decreases.When the medium pressure is 7.0×10^(5) Pa,the liquefaction capacity is 90.46 L/h,and the liquefaction efficiency reaches the maximum value of 18.6%.When the medium pressure is 12.5×10^(5) Pa,the liquefaction capacity and exergy efficiency are 107.4 L/h and 17.5%,respectively.Compared with the Modified-Claude cycle,the double-pressure cycle reduces the exergy destruction of the throttle valve and reduces the power consumption of the system,improving the overall exergy efficiency of the system.
作者 苏惠坤 李正宇 龚领会 张梅梅 SU Huikun;LI Zhengyu;GONG Linghui;ZHANG Meimei(State Key Laboratory of Technologies in Space Cryogenic Propellants,Technical Institute of Physics and Chemistry,Chinese Academy of Sciences,Beijing 100190,China;University of Chinese Academy of Sciences,Beijing 100190,China)
出处 《华中科技大学学报(自然科学版)》 EI CAS CSCD 北大核心 2024年第4期143-148,共6页 Journal of Huazhong University of Science and Technology(Natural Science Edition)
基金 中国科学院战略性先导科技专项资助项目(XDC10010000)。
关键词 氦液化器 液化循环 液化率 效率 (火用)分析 helium liquifier liquefaction cycle liquefaction rate efficiency exergy analysis
  • 相关文献

参考文献5

二级参考文献19

  • 1段欣悦,厉彦忠.低温流体节流过程空化现象的形成与发展规律[J].航天器环境工程,2009,26(6):554-560. 被引量:9
  • 2章洁平.液氢加注系统[J].低温工程,1995(4):25-28. 被引量:7
  • 3Utturkar Y,Wu J Y,Wang G Y, et al. Recent progress in modeling of cryogenic cavitation for liquid rocket pro- pulsion [ J]. Progress in Aerospace Sciences, 2005,41 : 558 - 608.
  • 4林畅达.平衡流量计标定系统的设计与研究:[硕士学位论文][D].上海:华东理工大学,2011.
  • 5Khalil A, McIntosh G E. Thermodynamic Optimization Study of the Helium Muttiengine Claude Refrigeration Cycle [J]. Advances in Cryogenic Engineering, 1978, 23:431- 437.
  • 6Minta M, Smith Jr J L. An Entropy Flow Optimization Technique for Helium Liquefaction Cycles. Advances in Cryogenic Engineering, 1984, 29:469 -478.
  • 7郭永样,甘智华,PfotenhauerJ.“控制体”方法分析液化循环的热力学问题讨论--以Claude循环为例[C]//第十二届全国低温工程大会论文集.南京,2015:194-202.
  • 8GUO Yongxiang, GAN Zhihua, Pfotenhauer J. Discussion on Thermodynamic Problem of Control Volume Method in Liquefaction Cycle Analysis [C]// Proceeding of The 12^th National Conference on Cryogenic Engineering, Nan- jing, 2015:194-202.
  • 9Thomas R J, Ghosh P, Chowdhury K. Role of Heat Ex- changers in Helium Liquefaction Cycles: Simulation Stud- ies Using Collins cycle [J]. Fusion Engineering and Design, 2012, 87(1): 39 -46.
  • 10Thomas R J, Ghosh P, Chowdhury K. Role of Expanders in Helium Liquefaction Cycles: Parametric Studies Using Collins Cycle [J]. Fusion Engineering and Design, 2011, 86(4): 318-324.

共引文献16

同被引文献36

引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部